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Hypersonic aerodynamic characteristics of a variable-dihedral delta-wing spacecraft configurationWind tunnel stability tests of variable dihedral delta wing spacecraft configuration at hypersonic speed
Document ID
19710024532
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ellison, J. C. (NASA Langley Research Center Hampton, VA, United States)
Spencer, B., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-2391
L-7752
Report Number: NASA-TM-X-2391
Report Number: L-7752
Accession Number
71N34008
Funding Number(s)
PROJECT: RTOP 117-07-01-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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